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Effect of combination of active and passive flow control methods on the flow structures and loss of a highly-loaded compressor cascade

  • Longxin Zhang
  • , Songtao Wang*
  • , Xun Liu
  • , Jun Ding
  • , Zhongqi Wang
  • *Corresponding author for this work
  • Harbin Institute of Technology
  • Harbin Boiler and Turbine Institute

Research output: Contribution to journalArticlepeer-review

Abstract

In order to simplify the aspirated structure and improve the engineering appliance of the aspirated compressor, a compound flow control method, composed of tandem cascade and endwall suction technology, is proposed. Effects of applying tandem cascade, endwall suction and compound flow control method on the flow structures and aerodynamic loss of a highly loaded outlet vane are investigated by numerical simulations. As a result, the control effect of the compound flow control method is advantageous over the single flow control method, the corner stall is depressed and the two-dimensional flow separation is alleviated effectively by using a smaller aspirated flow rate, moreover, the outlet flow parameters turn more evenly, the total pressure loss is reduced by 59% when 0.90% of inlet mass flow is sucked away.

Original languageEnglish
Pages (from-to)161-167
Number of pages7
JournalJixie Gongcheng Xuebao/Chinese Journal of Mechanical Engineering
Volume52
Issue number22
DOIs
StatePublished - 20 Nov 2016

Keywords

  • Aircraft engine
  • Boundary layer aspiration
  • Compound flow control method
  • Highly-loaded compressor
  • Tandem cascade

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